View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 39446U 13066AG 23089.42251903 .00006230 00000-0 77396-3 0 9996
2 39446 97.7262 47.0365 0064605 235.6783 123.8305 14.81439450502762
| Epoch (UTC): | 30 March 2023 10:08:25 |
| Eccentricity: | 0.0064605 |
| inclination: | 97.7262° |
| perigee height: | 579 km |
| apogee height: | 670 km |
| right ascension of ascending node: | 47.0365° |
| argument of perigee: | 235.6783° |
| revolutions per day: | 14.81439450 |
| mean anomaly at epoch: | 123.8305° |
| orbit number at epoch: | 50276 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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